### REFERENCE: TR22 Issue 1.0 AFM ISSUE DATE: 26 NOV 09



# A330/A340 TEMPORARY REVISION TR22 issue 1.0 

# - TR 4.02.00/40 ISSUE 2 - UNDETECTED ELEVATOR CONTROL LOSS IN CASE OF DUAL FAILURE 

# AIRPLANE FLIGHT MANUAL

The content of this document is the property of Airbus. It is supplied in confidence and commercial security on its contents must be maintained. It must not be used for any purpose other than that for which it is supplied, nor may information contained in it be disclosed to unauthorized persons. It must not be reproduced in whole or in part without permission in writing from the owners of the copyright. © AIRBUS 2005. All rights reserved.

AIRBUS S.A.S CUSTOMER SERVICES DIRECTORATE 31707 BLAGNAC CEDEX FRANCE

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TR22 Issue 1.0 PLP-TOC P 1 /2 AFM 26 NOV 09 

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### APPRO APPROVAL DATA APPRO-TR TEMPORARY REVISIONS (TR 4.02.00/40 Issue 2) - Undetected Elevator Control Loss in case of Dual Failure

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### ABN ABNORMAL PROCEDURES ABN-27 FLIGHT CONTROLS UNDETECTED ELEVATOR CONTROL LOSS IN CASE OF DUAL FAILURE

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### ABN-29 HYDRAULIC UNDETECTED ELEVATOR CONTROL LOSS IN CASE OF DUAL FAILURE

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TR22 Issue 1.0 PLP-TOC P 2/2 AFM 26 NOV 09A330/A340

AIRPLANE FLIGHT MANUAL 

### APPROVAL DATA TEMPORARY REVISIONS

TR22 Issue 1.0 APPRO-TR P 1 /2 AFM 26 NOV 09 

### TR22 Issue 1.0 (TR 4.02.00/40 ISSUE 2) - UNDETECTED ELEVATOR CONTROL LOSS IN CASE OF DUAL FAILURE Ident.: TDU / APPRO-TR-00009372.0001001 / 26 NOV 09 EASA APPROVED Criteria: (340-200 or 340-300) Impacted DU: NONE 

### APPROVAL REFERENCE APPROVED BY: EASA Approval date: 26 NOV 09 Approval reference: 10028037 Do not remove this Temporary Revision until instructed to do so. Reason for issue: This TRis issued in digital format to provide the content of TR4.02.00/40

Issue 2 approved by the EASA under reference 2004_9191 on September 2nd, 2004. Applicable to: A340-200 or A340-300 aircraft.

This Temporary Revision is made up of the following Temporary Documentary Units: APPRO-TR-00009372.0001001/26 NOV 09 ABN-29-00009373.0001001/26 NOV 09 ABN-27-00009371.0001001/26 NOV 09A330/A340 AIRPLANE FLIGHT MANUAL 

### APPROVAL DATA TEMPORARY REVISIONS



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TR22 Issue 1.0 APPRO-TR P 2/2 AFM 26 NOV 09A330/A340

AIRPLANE FLIGHT MANUAL 

### ABNORMAL PROCEDURES FLIGHT CONTROLS

TR22 Issue 1.0 ABN-27 P 1 /2 AFM 26 NOV 09 

### UNDETECTED ELEVATOR CONTROL LOSS IN CASE OF DUAL FAILURE
Ident.: TDU / ABN-27-00009371.0001001 / 26 NOV 09 EASA APPROVED Criteria: (340-200 or 340-300) Impacted DU: NONE Impacted by TR22 Issue 1.0 

### On ground, before takeoff until takeoff power thrust setting, apply the following procedure.  In the case of a F/CTL - PRIM 1 FAULT, or F/CTL - PRIM 1 PITCH FAULT: Turn off PRIM 1, then back on to perform a FCPC PRIM 1 reset.  If successful: Perform the normal pre-flight Flight Control check.  If unsuccessful: Return to the gate and require appropriate maintenance actions.  In the case of a F/CTL - ELEV SERVO FAULT: Return to the gate and require appropriate maintenance actions.A330/A340 AIRPLANE FLIGHT MANUAL 

### ABNORMAL PROCEDURES FLIGHT CONTROLS



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TR22 Issue 1.0 ABN-27 P 2/2 AFM 26 NOV 09A330/A340

AIRPLANE FLIGHT MANUAL 

### ABNORMAL PROCEDURES HYDRAULIC

TR22 Issue 1.0 ABN-29 P 1 /2 AFM 26 NOV 09 

### UNDETECTED ELEVATOR CONTROL LOSS IN CASE OF DUAL FAILURE
Ident.: TDU / ABN-29-00009373.0001001 / 26 NOV 09 EASA APPROVED Criteria: (340-200 or 340-300) Impacted DU: NONE Impacted by TR22 Issue 1.0 

### On ground, before takeoff until takeoff power thrust setting, apply the following procedure.  In the case of a HYD - G SYS LO PR: Return to the gate and require appropriate maintenance actions.A330/A340 AIRPLANE FLIGHT MANUAL 

### ABNORMAL PROCEDURES HYDRAULIC



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TR22 Issue 1.0 ABN-29 P 2/2 AFM 26 NOV 09